GB201016279D0 - Stiffener run-out - Google Patents

Stiffener run-out

Info

Publication number
GB201016279D0
GB201016279D0 GBGB1016279.0A GB201016279A GB201016279D0 GB 201016279 D0 GB201016279 D0 GB 201016279D0 GB 201016279 A GB201016279 A GB 201016279A GB 201016279 D0 GB201016279 D0 GB 201016279D0
Authority
GB
United Kingdom
Prior art keywords
stiffener
run
stiffener run
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
GBGB1016279.0A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations Ltd
Original Assignee
Airbus Operations Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Ltd filed Critical Airbus Operations Ltd
Priority to GBGB1016279.0A priority Critical patent/GB201016279D0/en
Publication of GB201016279D0 publication Critical patent/GB201016279D0/en
Priority to PCT/GB2011/051795 priority patent/WO2012042246A2/en
Priority to RU2013119649/11A priority patent/RU2562094C2/en
Priority to US13/820,619 priority patent/US10023293B2/en
Priority to EP11764264.5A priority patent/EP2621802B1/en
Priority to KR1020137009888A priority patent/KR20130139929A/en
Priority to CA2811031A priority patent/CA2811031A1/en
Priority to CN201180046623.7A priority patent/CN103124673B/en
Priority to JP2013530797A priority patent/JP2013544692A/en
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49616—Structural member making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24008—Structurally defined web or sheet [e.g., overall dimension, etc.] including fastener for attaching to external surface
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Moulding By Coating Moulds (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Body Structure For Vehicles (AREA)
  • Superstructure Of Vehicle (AREA)
  • Bridges Or Land Bridges (AREA)
  • Load-Bearing And Curtain Walls (AREA)
GBGB1016279.0A 2010-09-28 2010-09-28 Stiffener run-out Ceased GB201016279D0 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
GBGB1016279.0A GB201016279D0 (en) 2010-09-28 2010-09-28 Stiffener run-out
PCT/GB2011/051795 WO2012042246A2 (en) 2010-09-28 2011-09-22 Stiffener run-out
RU2013119649/11A RU2562094C2 (en) 2010-09-28 2011-09-22 Stiffening element edge line
US13/820,619 US10023293B2 (en) 2010-09-28 2011-09-22 Stiffener run-out
EP11764264.5A EP2621802B1 (en) 2010-09-28 2011-09-22 Stiffener run-out
KR1020137009888A KR20130139929A (en) 2010-09-28 2011-09-22 Stiffener run-out
CA2811031A CA2811031A1 (en) 2010-09-28 2011-09-22 Stiffener run-out
CN201180046623.7A CN103124673B (en) 2010-09-28 2011-09-22 Reinforcement is cut sth. askew position
JP2013530797A JP2013544692A (en) 2010-09-28 2011-09-22 Reinforcement relief

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1016279.0A GB201016279D0 (en) 2010-09-28 2010-09-28 Stiffener run-out

Publications (1)

Publication Number Publication Date
GB201016279D0 true GB201016279D0 (en) 2010-11-10

Family

ID=43128073

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB1016279.0A Ceased GB201016279D0 (en) 2010-09-28 2010-09-28 Stiffener run-out

Country Status (9)

Country Link
US (1) US10023293B2 (en)
EP (1) EP2621802B1 (en)
JP (1) JP2013544692A (en)
KR (1) KR20130139929A (en)
CN (1) CN103124673B (en)
CA (1) CA2811031A1 (en)
GB (1) GB201016279D0 (en)
RU (1) RU2562094C2 (en)
WO (1) WO2012042246A2 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8974886B2 (en) * 2012-04-25 2015-03-10 The Boeing Company Disbond resistant composite stiffener runout
GB201209439D0 (en) * 2012-05-28 2012-07-11 Airbus Operations Ltd A securing plate and aircraft structure
GB201209437D0 (en) * 2012-05-28 2012-07-11 Kitchener Renato Power supply and battery charger
EP2989003A4 (en) * 2013-04-25 2016-12-07 Saab Ab Stiffening element run-out
ES2819076T3 (en) * 2013-04-30 2021-04-14 Airbus Operations Sl Composite structure for an aircraft and its manufacturing process
JP6169465B2 (en) 2013-10-02 2017-07-26 三菱重工業株式会社 Joints and aircraft structures
US10086922B2 (en) 2013-11-15 2018-10-02 The Boeing Company Low stress stiffener runout in Pi bonded structure
GB201511402D0 (en) 2015-06-30 2015-08-12 Short Brothers Plc Repair including a chamfered bracket and a chamfered bracket component for reinforcing a damaged structural element made from composite materials
GB2565351A (en) * 2017-08-11 2019-02-13 Airbus Operations Ltd Panel assembly
GB2565350A (en) 2017-08-11 2019-02-13 Airbus Operations Ltd Panel assembly
US11724791B2 (en) 2019-10-08 2023-08-15 The Boeing Company Enhanced design for stringer runout terminations on composite panels

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830581A (en) 1972-05-26 1974-08-20 Ecodyne Corp Green wood joint
GB2072579B (en) 1980-04-01 1984-06-06 British Aerospace Stiffened panel of fibre reinforced plastics materials
US4507011A (en) 1982-05-03 1985-03-26 The Boeing Company Reinforced elastomer attachment joint
FR2533013B1 (en) 1982-09-09 1986-05-30 Alkan R & Cie METHOD FOR IMPLANTING A METAL REINFORCEMENT IN A FIBER-RESIN COMPOSITE MATERIAL STRUCTURE
RU2112698C1 (en) * 1996-09-30 1998-06-10 Обнинское научно-производственное предприятие "Технология" Panel made from composite material
FR2866626B1 (en) 2004-02-20 2006-05-19 Airbus France OFFSET OF STIFF SLITTED SLOPES AND PANEL PROVIDED WITH SUCH A STOP
GB0525896D0 (en) 2005-12-20 2006-02-01 Airbus Uk Ltd A joint for use in aircraft construction
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
GB0708333D0 (en) 2007-04-30 2007-06-06 Airbus Uk Ltd Composite structure
DE102007063608B4 (en) 2007-05-23 2011-04-21 Airbus Operations Gmbh Composite and fuselage cell section with such a composite
ATE495006T1 (en) 2007-05-31 2011-01-15 Airbus Operations Gmbh METHOD FOR PRODUCING A COMPOSITE SKIN IN THE AEROSPACE FIELD
DE102007029500B4 (en) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Method for coupling stiffening profile elements and structural component
FR2922517B1 (en) * 2007-10-18 2010-04-23 Airbus France AIRCRAFT COMPRISING SUNNY ARRESTOR JUNCTIONS AND METHOD OF MANUFACTURING SUCH A PLANE
DE102008010197B4 (en) 2008-02-20 2012-03-22 Airbus Operations Gmbh Method for connecting two fuselage sections with the creation of a transverse joint and transverse joint connection
DE102008012252B4 (en) 2008-03-03 2014-07-31 Airbus Operations Gmbh Composite as well as aircraft or spacecraft with such a composite
US8540833B2 (en) * 2008-05-16 2013-09-24 The Boeing Company Reinforced stiffeners and method for making the same
DE102008002117B4 (en) * 2008-05-30 2013-10-31 Airbus Operations Gmbh Composite and structure
DE102008041172B9 (en) 2008-08-12 2014-03-13 Airbus Operations Gmbh Aircraft with a fuselage structure with welded skin panels
GB0819159D0 (en) 2008-10-20 2008-11-26 Airbus Uk Ltd Joint between aircraft components
DE102009013585B4 (en) * 2009-03-17 2012-01-26 Airbus Operations Gmbh Fuselage cell structure for a hybrid aircraft
US8993084B2 (en) 2010-08-17 2015-03-31 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US8652606B2 (en) 2010-08-17 2014-02-18 The Boeing Company Composite structures having composite-to-metal joints and method for making the same
ES2398985B1 (en) 2011-03-14 2014-02-14 Airbus Operations S.L. LOAD TRANSFER DEVICES IN THE TERMINATION OF A LARGUERILLO.

Also Published As

Publication number Publication date
US10023293B2 (en) 2018-07-17
CN103124673A (en) 2013-05-29
CN103124673B (en) 2016-04-27
EP2621802B1 (en) 2016-11-09
EP2621802A2 (en) 2013-08-07
US20130164489A1 (en) 2013-06-27
WO2012042246A2 (en) 2012-04-05
KR20130139929A (en) 2013-12-23
WO2012042246A3 (en) 2012-06-21
RU2562094C2 (en) 2015-09-10
JP2013544692A (en) 2013-12-19
CA2811031A1 (en) 2012-04-05
RU2013119649A (en) 2014-11-10

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)